Method for interpreting events of seismic records to yield indications of gaseous hydrocarbons

ABSTRACT

The present invention indicates that gas-containing strata of an earth formation have low Poisson&#39;s ratios and that the acoustic contrast with the overburden rock has a surprising effect as a function of the angle of incidence on a seismic wave associated with an array of sources and detectors: viz., a significant--and progressive--change in P-wave reflection coefficient as a function of the angle of incidence occurs. Thus, differentiating between high-intensity amplitude annomalies of nongas- and gas-containing media is simplified: progressive change in amplitude intensity of resulting traces generated by the field array as a function of offset between each source-detector pair, is associated with the last-mentioned medium only.

RELATED APPLICATION

This application is a continuation-in-part of U.S. Ser. No. 756,584, filed Jan. 3, 1977, for "Method for Interpretation of Seismic Records to Yield Indications of Gaseous Hydrocarbons" now abandoned.

FIELD OF THE INVENTION

The present invention pertains to the art of seismic prospecting for petroleum reservoirs by multiple-point surveying techniques, and more particularly to the art of converting high-intensity reflection amplitude anomalies associated with one or more common centerpoints observed on seismic record traces into diagnostic indicators of the presence of gas in the underlying subsurface strata.

BACKGROUND OF THE INVENTION

For several decades, seismic prospecting for petroleum has involved the creation of acoustic disturbances above, upon, or just below the surface of the earth, using explosives, air guns, or large mechanical vibrators. Resulting acoustic waves propagate downwardly in the earth, and are partially reflected back toward the surface when acoustic impedance changes within the earth are encountered. A change from one rock type to another, for example, may be accompanied by an acoustic impedance change, so that the reflectivity of a particular layer depends on the velocity and density content between that layer and the layer which overlies it, say according to the formula ##EQU1## where AR is the amplitude from the reflected signal and Ai is the amplitude of the incident signal: V₁ is the velocity of the wave in the overlying medium 1; V₂ is the velocity in the medium layer below the contact line; d₁ is the density of the overlying medium 1; and d₂ is the density of the underlying medium.

In early years, signal traces of the reflected acoustic waves were recorded immediately in the field as visible, side-by-side, dark, wiggly lines on white paper ("seismograms"). At present, the initial reproductions--in a digital format--are on magnetic tape, and finally are reduced to visible side-by-side traces on paper or film in large central computing facilities.

At such centers, sophisticated processing makes possible the distinction of signals from noise in cases that would have seemed hopeless in the early days of seismic prospecting. Until 1965, almost all seismic surveys conducted used an automatic gain control which continuously adjusted the gain of amplifiers in the field to account for decreasing amounts of energy from late reflection arrivals. As a result, reflection coefficients could not be accurately determined. However, with the advent of the expander circuit and binary gain amplifiers, gain of the amplifiers can now be controlled and amplitudes recorded precisely; this makes it possible to conserve not only the special characteristics of the reflections, but also their absolute amplitudes.

There was also another problem in the prior art equipment. Computers often precluded the use of a comparison technique because of their small word size and tiny core storage. Today, more powerful computers with array processors and economical floating point capabilities now enable modern geophysicists to maintain control of the amplitude of all recorded signals. The "floating point" capability is especially effective in expanding computer work size by a large factor and in eliminating the need for computer automatic gain control.

That is to say, in summary, as a result of the above advances, reflections from many thousands of feet below the earth's surface can now be confidently detected and followed through sometimes hundreds of side-by-side traces, the shortening or lengthening of their corresponding times of arrival being indicative of the shallowing or deepening of actual sedimentary strata of interest. Still, as a general rule, all that can be hoped for the seismic reflection method is to detect stratigraphic interfaces and the interfaces as they deviate from horizontality of these interfaces, so that subsurface "structures" could be defined in which oil or gas might possibly be trapped.

Apropos of the above has been use of ultra-high amplitude anomalies in seismic traces to infer the presence of natural gas in situ. Seismic interpretators have used so-called "bright-spot" analysis to indicate several large gas reservoirs in the world, especially in the Gulf Coast of the United States. Such analysis is now rather common in the oil industry, but it is not without its critics. Not only cannot the persistence of such increased amplitude anomalies be taken as confirmation of the lateral extent of the gas reservoir, but also the anomaly itself (in some cases) may not represent reflections of a discontinuity of a gas-bearing medium and its over- or underlying associated rock strata. E.g., experience has shown that in certain situations, similar phenomena occur which can confuse the interpreter. E.g., if the shape of the horizon is such that it focuses the energy back to the surface, it may increase the amplitude of one or more of the records akin to reflections from gas-saturated strata. Lithology of the horizon--singly and in combination--can also have a similar effect, producing high-amplitude reflections in the absence of gas within the pore space of the stratum of interest. Examples of the latter: conglomeratic zones, hard streaks of silt or lime and lignite beds.

The present invention improves the ability of the seismologist to correctly differentiate high-intensity anomalies of multiple-point-coverage seismic traces of gas-bearing strata from those of similarly patterned reflections of other types of stratigraphic configurations containing no gas accumulations.

OBJECT OF THE INVENTION

An object of the invention is the provision of a novel method of correctly differentiating high-intensity anomalies provided by multiple-point seismic traces of gas-bearing structures from those of a similarly patterned intensity associated with strata containing no gas accumulation.

SUMMARY OF THE INVENTION

In accordance with the present invention, interpretation of high-intensity seismic events from traces obtained from multiple-point coverage of a subterranean earth formation using an array of source means and detectors adjacent to the earth's surface is obtained to indicate gas-bearing strata in a highly surprising and accurate manner. After the field data have been obtained in which the data of common centerpoints are associated with more than one source-detector pair, the data are indexed whereby all recorded traces are indicated as being a product of respective source-detector pairs of known horizontal offset and centerpoint location. Thereafter, high-intensity amplitude anomalies in said traces are correctly associated with gas-bearing strata on a surprisingly accurate selection basis: amplitude intensity of said anomaly must change--progressively in an increasing or decreasing manner--as a function of horizontal offset. A further refinement of the method of the present invention may be in order under some circumstances. A single common-centerpoint trace, or even single common-centerpoint gathers, may have a major drawback in such cases--poor signal-to-noise ratios. As a result, progressive amplitude change as a function of offset cannot be resolved. In accordance with this invention and as a means of signal enhancement, trace summations can prove beneficial in improving record resolution, say on a basis of combining a group of traces having a two-dimensional axes for addressing the traces: progressively increasing common horizontal offset and common centerpoint location. Where 2400% common-centerpoint stacked traces have been obtained (i.e., 24 traces per gather) by multiple-point-coverage field techniques, each gather can in turn be "destacked" to provide original but corrected locational traces. Then on the basis of progressive changes in offset and centerpoint location, several such traces, say 10, can be stacked and the stacked trace displayed as a function of offset. Result: progressive change in amplitude intensity as a function of similar intensity changes in offset can be more easily observed whereby in situ gas is, more likely than not, in the pore space of the structure of interest.

DESCRIPTION OF THE DRAWINGS

Further features of the invention will become more apparent upon consideration of the following detailed description of the invention when taken in connection with the accompanying drawings, wherein:

FIG. 1 is a plan view of a grid of centerpoints produced in the field by the systematic positioning and energization of an array of seismic sources and detectors whereby a series of locational traces associated with individual centerpoints between respective source-detector pairs are ultimately generated;

FIG. 2 is a model of typical reflecting horizons within an earth formation that can be associated with the characteristics of the locational traces of FIG. 1;

FIGS. 3, 4 and 5 are plots of reflection coefficient as a function of angle of incidence of seismic waves associated with the reflecting horizons of FIG. 2 which aid in the determination of the presence of gas within an earth formation;

FIGS. 6(a), 6(b), 6(c) and 6(d) are plots of various quantities of a mathematical nature, as a function of percentage of gas saturation, illustrating the relationship of Poisson's ratio to the determination of the presence of gas within an earth formation;

FIGS. 7 and 8 are plots of centerpoints produced by an array of sources and detectors wherein a geometrical transformation has occurred to better illustrate processes associated with the method of the present invention;

FIGS. 9(a) and 9(b) are flow diagrams of processes akin to those shown in FIGS. 7 and 8 for carrying out the method of the present invention, using a programmed digital computing system;

FIGS. 10 and 11 are schematic diagrams of elements within the digital computing system of FIG. 9;

FIGS. 12-21 are true seismic record sections and portions of sections, illustrating the diagnostic capability of the method of the present invention in predicting the presence of gas strata in actual field examples, and

FIGS. 22-25 are functional block diagrams of yet another embodiment of the present invention.

PREFERRED EMBODIMENTS OF THE INVENTION

Before discussion of an embodiment of the invention within an actual field environment, a brief description of the mathematical and theoretical concepts behind it may prove beneficial and are presented below.

Firstly, it may be of interest to indicate lithology limitations associated with the present invention. For example, anomalies associated with gas sands over shale cap rock are one example in which the method of the present invention offers surprising results; another relates to gas-saturated limestone over shale. Also of import is the relationship between Poisson's ratio and resulting high-intensity amplitude anomalies provided on seismic traces.

While Poisson's ratio () has the general formula ##EQU2## where Vp is compressional velocity and Vs is shear velocity of the medium, the concept does have physical significance. For example, consider a slender cylindrical rod of an elastic material and apply a compressional force to the ends. As the rod changes shape, the length of the rod will decrease by ΔL, while the radius will increase by ΔR. Poisson's ratio is defined as the ratio of the relative change in radius (ΔR/R) to the relative change in length (ΔL/L). Hence a compressible material has a low Poisson's ratio, while an incompressible material (as a liquid) has a high Poisson's ratio.

The equation above also indicates the relationship of the compressional and shear wave velocities of the material, Vp and Vs respectively; i.e., that Poisson's ratio may be determined dynamically by measuring the P-wave and S-wave velocities. Only two of the three variables are independent, however.

Recent published studies on reflection and transmission seismic waves useful in geophysical applications include:

(1) Koefoed, O., 1955, for "On the Effect of Poisson's Ratios of Rock Strata in the Reflection Coefficients of Plane Waves", Geophysical Prospecting, Vol. 3, No. 4.

(2) Koefoed, O., 1962, for "Reflection and Transmission Coefficients for Plane longitudinal Incident Waves", Geophysical Prospecting, Vol. 10, No. 3.

(3) Muskat, M. and Meres, M. W., 1940, for "Reflection and Transmission Coefficients for Plane Waves in Elastic Media", Geophysics, Vol. 5, No. 2.

(4) Tooley, R. D., Spencer, T. W. and Sagoic H. F., for "Reflection and Transmission of Plane Compressional Waves", Geophysics, Vol. 30, No. 4 (1956).

(5) Costain, J. K., Cook, K. L. and Algermisshi, S. T., for "Amplitude, Energy and Phase Angles of Plane SP Waves and Their Application to Earth Crustal Studies", Bull. Seis. Soc. Am., Vol. 53, p. 1639 et. seq.

All of the above have focused on the complex modeling of variation in reflection and transmission coefficients as a function of angle of incidence.

The problem is complicated, however. E.g., isotropic media with layer index of the strata, i=1 for the incident medium and i=2 for the underlying medium, have been modeled using equations for P-wave reflection coefficient Apr and for P-wave transmission displacement amplitude coefficient Apt. In such equations, the value of Poisson's ratio (σ) is required, since both the P-wave and S-wave velocities are utilized. For each of the media, i.e., the incident or underlying medium, three independent variables exist: P-wave velocity, σ and bulk density, or a total of six variables for both media. But for a single interface, only four independent variables were required: P-wave velocity ratio, the density ratio, Poisson's ratio in the incident medium and Poisson's ratio in the underlying medium.

But to provide for the many combinations of possible variations, the above-listed studies have either:

(a) generated many (literally thousands) plots of a mathematical nature for various parameters, values in which there was little relationship with true geophysical applications, since the latter were hopelessly obscured and unappreciated; or

(b) made simplistic assumptions that, although using actual calculations, nevertheless did not express the true nature of transmission and reflection coefficients, in particular lithological situations associated with the accumulation of gaseous hydrocarbons within an actual earth formation.

In summary, while reference (2) concluded that change in Poisson's ratio in the two bounding media can cause change in the reflection coefficient as a function of angle of incidence, (2) did not relate that occurrence to lithology associated with the accumulation of gaseous hydrocarbons in the surprising manner of the present invention.

The present invention teaches that gas-containing strata have low Poisson's ratios and that the contrast with the overburden rock as a function of horizontal offset produces a surprising result: such contrast provides for a significant--and progressive--change in P-wave reflection coefficient at the interface of interest as a function of angle of incidence of the incident wave. Thus, differentiating between high-intensity amplitude anomalies of nongas and gas media is simplified by relating progressive change in amplitude intensity as a function of offset between source-detector pairs, i.e., angle of incidence being directly related to offset.

Also, the behavior of P-wave travel as a function of lithology and horizontal offset between a respective source-detector pair associated with a given locational trace provide the following amplitude response signatures of interest:

(1) where the gas-containing media are gas sands underlying shale, such as found in the Gulf Coast, amplitude responses increase with offset;

(2) where the gas-containing media include limestone underlying shale, such as found in the North Sea, the amplitude anomalies of the interface decrease with offset.

Now in more detail, attention should be directed to the Figures, particularly FIG. 1. Note that, inter alia, FIG. 1 illustrates in some detail how the terms of interest in this application are derived: e.g., the term "centerpoint" is a geographical location located midway between a series of sources S₁,S₂ . . . Sn of a geophysical field system 9 and a set of detectors D₁,D₂ . . . Dm at a datum horizon near the earth's surface. The centerpoints are designated C₁,C₂ . . . Cp in the Figure, and are associated with a trace derived by placement of a source at that centerpoint location followed immediately by relocating a detector thereat.

I.e., if the sources S₁ . . . Sn are excited in sequence at the source locations indicated, traces received at the different detector locations shown can be related to common centerpoints therebetween. If such traces are summed, a gather or group of traces is formed. I.e., if the reflecting interface is a flat horizon, the depth point where reflection occurs will define a vertical line which passes through the centerpoint of interest. Applying static and dynamic corrections to the field traces is equivalent (under the above facts) to placing the individual sources S₁,S₂ . . . Sn at the centerpoint in sequence followed by replacement with the detectors D₁ . . . Dm of interest at the same locations. If the traces associated with a common centerpoint are summed, a series of enhanced traces, sometimes called CDPS (Common Depth Point Stack) traces, is provided.

FIG. 2 illustrates reflection phenomena of a three-layer model typical of a young, shallow geologic section 10, such as found in the Gulf Coast, illustrating how reflection phenomena associated with the traces associated with the field system 9 of FIG. 1 can be related to the presence of gas.

Section 10 includes a gas sand 11 embedded in a shale stratum 12. Assume a Poisson's ratio of 0.1 for the gas sand and of 0.4 for the shale, a 20% velocity reduction at interface 13, say from 10,000'/sec to 8000'/sec, and a 10% density reduction from 2.40 g/cc to 2.16 g/cc.

The actual P-wave reflection coefficient Apr can be related to section 10 by Equation (1) below; also, P-wave transmission displacement amplitude coefficient Apt can similarly be related in accordance with Equation (2) below. ##EQU3##

Equations (1) and (2) are, of course, the two basic equations of wave travel in an earth formation and are for isotropic media with the layer index being i=1 for the incident medium and i=2 for the underlying medium. Equations (3) through (17) simply define intermediate variables.

As an example of calculations associated therewith, if θ=0° (normal incidence), the P-wave reflection coefficient Apr is equal to about -0.16 and +0.16, respectively.

FIG. 3 illustrates change in reflection coefficient as a function of angle of incidence θ for the three-layer model of FIG. 2.

Note that solid lines 20, 21 illustrate the effects of reflection (and transmission, by omission) on the top and base of the gas sand. In line 20, at θ=0°, note that the Apr equals -0.16; while at θ=40°, the Apr is about -0.28. That is, rather a surprisingly large change in the reflection coefficient as a function of angle of incidence occurs, with the greatest change occurring between θ=20° and θ=40°.

For the bottom layer, line 21 changes at about the same rate, but in opposite sign. I.e., at θ=0°, Apr is about +0.16 and at θ=40°, Apr is about +0.26. Again, the greatest change in Apr occurs between θ=20° and θ=40°. As a result, the amplitude of the seismic wave reflected from this model would increase about 70% over the angle of incidence range shown, i.e., over the incremental 40 degrees shown.

While angles of incidence equal to 40° may seem a little large for reflection profiling (heretofore, most data arriving beyond 30° being thought useless and muted out), experience has now nevertheless shown that reflection data can and do arrive at reflection angles greater than 30°. Hence, the angles of incidence must be determined, and one of the more important techniques, the straight-ray approach to estimate such angles of incidence (using depth-to-reflector and shot-to-detector and-shot-to-group offset), is as set forth below:

    θ.sub.1 =arc tan (X/2Z)                              (18)

where θ₁ is the angle of incidence; X is the shot-to-detector or shot-to-group offset and Z is the reflector depth. Velocity changes with depth can likewise be accommodated by assuming section velocity change is of the form V₁ =V_(o) +KZ where K is a constant so that all ray paths are arcs of circles having centers V_(o) /K above the reference plane of interest, say the earth's surface. Thus, the approach should be in accordance with ##EQU4##

Having now established a firm mathematical and theoretical basis for the process of the present invention, perhaps a description of how a geological section containing no gas therein would affect impedance contrast is in order. FIG. 4 illustrates the changes in reflection coefficient as a function of angle of incidence θ in the manner of FIG. 3, but in which the gas sand 10 of FIG. 2 contains no gas, simulating, e.g., a low-velocity, brine-saturated, young sandstone embedded in shale.

The solid lines 22, 23, representing reflection coefficients, are seen to be about horizontal between θ=0° and 40°, slightly decreasing in magnitude as the angle of incidence increases, i.e., as θ approaches 40°. In the above example, it should be noted that the Poisson's ratio of the sandstone was assumed to be 0.4.

FIG. 5 illustrates yet another plot associated with a three-layer model akin to that shown in FIG. 2, but in which the sandstone contains gas but is buried deep below the earth's surface. The values for the three-layer model of FIG. 2 are again used except that the velocity change from shale to sand is only 10%, or from 10,000'/sec to 9000'/sec. As shown, curves 25, 26 are even more significant: both curves are seen to increase in magnitude from over the 40° of change in the angle of incidence. However, field results have not verified these results, since Poisson's ratio in such gas sands may be strongly affected by depth, and not be as low as is now surprisingly taught by the present invention.

FIGS. 6(a), 6(b), 6(c) and 6(d) offer a possible explanation for low Poisson's ratio in gas-containing strata in general and in gas sands in particular. In the Figures, various quantities are plotted as a function of percentage of gas saturation. In FIG. 6(a), P-wave velocity is so plotted; in FIG. 6(b), S-wave velocity is depicted; in FIG. 6(c), the ratio of Vp/Vs is the value of interest; and in FIG. 6(d), Poisson's ratio is shown as a function of percent gas saturation.

Note that FIGS. 6(a) and 6(b) are for sandstones buried at 6000 feet with 35% porosity. FIGS. 6(c) and 6(d) result from FIGS. 6(a) and 6(b) using appropriate equations. But in FIG. 6(d), Poisson's ratio drops from about 0.3 to 0.1 from 0% to 10% gas saturation; on the other hand, the same ratio changes very little from 10% to 100% gas saturation (average value is about 0.09).

Hence, from the above mathematical and theoretical concepts, displays of reflection data can now be used to indicate change in reflection coefficient as a function of angle of incidence to indicate the presence of gaseous hydrocarbons. Such data are also now conveniently available, say using today's conventional field-gathering techniques involving multiple-area coverage, since the former can be derived from and is compatible with one of today's conventional forms of recorded reflection seismic data: common-depth-point (CDP) gathers. And, progressive changes in reflection amplitude vs. shot-to-detector (group) offset can form the basis of such a determination, since offset of any particular source-detector pair is directly related to the angle of incidence in accordance with Equation (19), supra.

But corrected locational trace data, before stacking in accordance with CDPS techniques, often have poor signal-to-noise ratios. Thus, changes in amplitude vs. offset may be difficult to observe in such data.

FIG. 7 is a diagram which illustrates a data "addressing" technique which improves amplitude versus offset resolution in such situations; in the Figure, the traces were generated using an end-shooting array of 48 detectors with source and detectors advancing one detector interval per shot point. Result: a 24-fold CDP-stacked record section was generated. Note further: each centerpoint is associated with 24 separate traces of varying offset.

In order to geometrically associate each generated locational trace with its common centerpoint, address guidance, as provided by FIG. 7, is important. To understand the nature of FIG. 7, assume that the sources S₁,S₂ . . . Sn are sequentially located at shotpoints SP₁,SP₂ . . . SPn at the top of the Figure. Assume also that the detectors are placed in line with the sources, i.e., along the same line of survey A at the detector locations D₁,D₂ . . . Dm. After each source is activated, reflections are received at the detectors, at the locations shown. Then by the "rollalong" technique, the source and detector spreads can be moved in the direction B of survey line A and the process repeated to provide a series of traces. The latter are associated with centerpoints midway between the respective detector-source pairs. In the Figure, assume source S₁ has been located at shotpoint SP₁ and excited. Midway between SP₁ and each of the detectors, at D₁, D₂ . . . Dm, is a series of centerpoints C₁, C₂ . . . Cn. The latter are each associated with a trace. In this regard and for a further description of such techniques, see U.S. Pat. No. 3,597,727 for "Method of Attenuating Multiple Seismic Signals in the Determination of Inline and Cross-Dips Employing Cross-Steered Seismic Data", Judson et al, issued Aug. 3, 1971, and assigned to the assignee of the present application. With appropriate static and dynamic corrections, the data can be related to the common centerpoints midway between individual source points and detectors, as discussed in the above-noted reference.

But by such a field technique, data provided generate 24 separate traces assoicated with the same centerpoint C₁ . . . Cn. In order to index ("address") these traces as a function of several factors including horizontal offset and centerpoint location, a stacking chart 44 as shown in FIG. 8 has been developed.

Chart 44 is a diagram in which a trace is located along a plurality of oblique common profile lines PL₁,PL₂ . . . , between a series of common offset and centerpoint locations at 90 degrees to each other. For best illustration, focus on a single shotpoint, say SP₁, and on a single detector spread having detectors D₁,D₂ . . . Dm of FIG. 8 along survey line A. Assume a source is located at shotpoint SP₁ and activated thereafter. The detector spread and source are "rolled" forward along survey line A in the direction B, being advanced one station per activation. Then after detection has occurred, and if the resulting centerpoint pattern is rotated 45° about angle 46 to profile line PL₁ and projected below the spread as in FIG. 8 as a function of common offset values and centerpoint positions, the chart 44 of FIG. 8 results. Of course, each centerpoint has an amplitude vs. time trace associated therewith, and for didactic purposes that trace can be said to project along a line normal to the plane of the Figure.

It should be emphasized that the centerpoints provided in FIGS. 7 and 8 are geographically located along the line of survey A in line with the source points SP₁,SP₂ . . . . As the locational traces are generated, the chart 44 aids in keeping a "tag" on each resulting trace. As the detector spread and sources are rolled forward one station and the technique repeated, another series of traces is generated associated with centerpoints on new profile line PL₂. That is, although the centerpoints are geographically still associated within positions along the survey line A of FIG. 7, by rotation along the angle 46, the new centerpoint pattern C₁ ',C₂ ' . . . Cn' can be horizontally and vertically aligned with centerpoints previously generated. I.e., at common offset values (in horizontal alignment) certain centerpoints are aligned, viz, centerpoint C₁ aligns with C₁ ' as shown; further C₂ is aligned with C₂ ', etc. Also, there are traces that have common centerpoints. I.e., at common centerpoints (in vertical alignment) centerpoint C₂ aligns with centerpoint C₁ ', and centerpoints C₃,C₂ ' and C₁ " are similarly aligned. Thus, via chart 44, each trace associated with a centerpoint can be easily "addressed" as to:

(i) its actual geographical location (i.e., along phantom lines normal to diagonal profile lines PL₁,PL₂ . . . along common location lines LL₁,LL₂ . . . ), so that its actual field location is likewise easily known;

(ii) its association with other traces along common horizontal offset lines COL₁,COL₂ . . . COLx; and

(iii) its association with still other traces along common vertical centerpoint location lines CPL₁,CPL₂ . . . .

Also, "addressing" the traces by (ii) and (iii) allows such traces to be easily combined (summed) by calling out "windows" within the chart in which any traces within the window can be summed. E.g., it has been found convenient to establish a standard window "width" equal to an increased group centerpoint line (-CPL) value of say 5, and a window "height" equal to an incremental common group offset line (-COL) value of say 4; hence by indexing the intersecting window intervals on a sequential basis, summation of traces therein can occur. The results are summed traces which are outputted to a display on a side-by-side basis, say as a function of amplitude intensity as a function of increasing or decreasing offset between respective source-detector pairs. Actual offset values are not required, since relative values are usually sufficient for most diagnostic purposes.

In carrying out the above summation process on a high-speed basis, a fully programmed digital computer can be useful. By electromechanical systems well known in the art can also be used. In either case, the field traces must first undergo static and dynamic correction before the traces can be displayed as a function of offset to determine their potential as a gas reservoir. Such correction techniques are well known in the art--see, e.g., U.S. Pat. No. 2,838,743, of O. A. Fredriksson et al, for "Normal Moveout Correction with Common Drive for Recording Medium and Recorder and/or Reproducing Means", assigned to the assignee of the present application, in which a mechanical device and method are depicted. Modern processing today uses properly programmed digital computers for that task in which the data words are indexed as a function of, inter alia, amplitude, time, datum height, geographical location, group offset, velocity, and are manipulated to correct for the angular and horizontal offset; in this latter environment, see U.S. Pat. No. 3,731,269, Judson et al, issued May 1, 1973, for "Static Corrections for Seismic Traces by Cross-Correlation Method", a computer-implemented program of the above type also assigned to the assignee of the present invention. Electromechanical sorting and stacking equipment is also well known in the art and is of the oldest ways of cancelling noise. See, for example, the following patents assigned to the assignee of the present invention which contain sorting and stacking techniques, including beam steering techniques:

    __________________________________________________________________________     Patent                                                                               Issued                                                                               Inventor                                                                               Title                                                      __________________________________________________________________________     3,597,727                                                                            12/30/68                                                                             Judson et al                                                                           Method of Attenuating Multiple                                                 Seismic Signals in the Deter-                                                  mination of Inline and Cross                                                   Dips Employing Cross-Steered                                                   Seismic Data                                               3,806,863                                                                            4/23/74                                                                              Tilley et al                                                                           Method of Collecting Seismic                                                   Data of Strata Underlying                                                      Bodies of Water                                            3,638,178                                                                            1/25/72                                                                              Stephenson                                                                             Method for Processing Three-                                                   Dimensional Seismic Data to                                                    Select and Plot Said Data on                                                   a Two-Dimensional Display                                                      Surface                                                    3,346,840                                                                            10/10/67                                                                             Lara    Double Sonogramming for                                                        Seismic Record Improvement                                 3,766,519                                                                            10/16/73                                                                             Stephenson                                                                             Method for Processing Surface                                                  Detected Seismic Data to                                                       Plotted Representations of Sub-                                                surface Directional Seismic Data                           3,784,967                                                                             1/8/74                                                                              Graul   Seismic Record Processing Method                           3,149,302                                                                            9/15/74                                                                              Klein et al                                                                            Information Selection Programmer                                               Employing Relative Amplitude,                                                  Absolute Amplitude and Time                                                    Coherence                                                  3,149,303                                                                            9/15/64                                                                              Klein et al                                                                            Seismic Cross-Section Plotter                              __________________________________________________________________________

FIGS. 9(a) and 9(b) are flow diagrams illustrative of a computer-dominated process in which the functions required by the method of the present invention can be easily ascertained. Preliminary to the steps shown in FIG. 9(a), assume that a section of seismic data has been analyzed for "bright spots"; such events are known by geographical location and/or a time/depth basis; and the traces have been dynamically and statically corrected.

The steps of FIG. 9(a) include generating addresses for the data that include a common offset address in the manner of FIG. 8, common centerpoint address and an actual geographical location address in the manner of FIG. 8. Finally, the corrected traces are classified whereby the amplitude event of interest is displayed as a function of changing horizontal offset valves. If the event progressively changes as a function of offset, there is a high likelihood that the event is indicative of strata containing gaseous hydrocarbons.

After the addresses have been generated, trace amplitude summation can also occur as suggested in FIG. 9(b) on a predetermined selection basis: adding traces within a selected "window", say window 49 bounded by common group centerpoint lines (ΔCPI) and common group offset lines (ΔCOL) (see FIG. 8), usually the "width" (ΔCPI) of window 49 is held constant, and the window "height" (ΔCCI) is incremented, frame-by-frame, to change common offset values on a progressive basis, say from near offset values to far offset values. E.g., in FIG. 8, holding the window "width" constant and beginning at the lower boundary of the chart 44, the window "height" (ΔCOL) can be incremented until the upper plot boundary is reached. Equipment-wise, the addresses of the boundary lines in the line and column directions are compared--within each window frame. When the comparison is a match, the address register is incremented, and the process repeated for the next window frame.

After the summed traces are tagged on the basis of changing common offset, say near through far offset, summed traces can be displayed. If the amplitudes exhibit the required characteristics, as previously stated, then a determination that the reflections are from (or not from) a gas structure can be made.

Of course, if the edge of a gas field is to be determined, the above-mentioned process would be sequentially elongated toward a side of the chart 44 of FIG. 8 in a direction along the survey line. I.e., to say, after the window "height" has been incremented to its far offset value and the results displayed, the window "width" is incremented a common group centerpoint interval (ΔCPL) and the process repeated and the results displayed.

FIG. 10 illustrates particular elements of a computing system for carrying out the steps of FIGS. 9(a) and 9(b). While many computing systems are available to carry out the process of the invention, perhaps to best illustrate operations at the lowest cost per instruction, a microcomputing system 50 is didactically best and is presented in detail below. The system 50 of FIG. 10 can be implemented on hardware provided by many different manufacturers, and for this purpose, elements provided by Intel Corporation, Santa Clara, Calif., may be preferred.

Such a system 50 can include a CPU 51 controlled by a control unit 52. Two memory units 53 and 54 connect to the CPU 51 through BUS 55. Program memory unit 53 stores instructions for directing the activities of the CPU 51 while data memory unit 54 contains data (as data words) related to the seismic data provided by the field acquisition system. Since the seismic traces contain large amount of bit data, an auxiliary memory unit 56 can be provided. The CPU 51 can rapidly access data stored through through addressing the particular input port, say at 57a in the Figure. Additional input ports can also be provided to receive additional information as required from usual external equipment well known in the art, e.g., floppy disks, paper-tape readers, etc., including such equipment interfaced through input interface port 57b tied to a keyboard unit 58 for such devices. Using clock inputs, control circuitry 52 maintains the proper sequence of events required for any processing task. After an instruction is fetched and decoded, the control circuitry issues the appropriate signals (to units both internal and external) for initiating the proper processing action. Often the control circuitry will be capable of responding to external signals, such as an interrupt or wait request. An interrupt request will cause the control circuitry 52 to temporarily interrupt main program execution, jump to a special routine to service the interrupting device, then automatically return to the main program. A wait request is often issued by memory units 53 or 54 or an I/O element that operates slower than the CPU.

For outputting information, the system 50 can include a printer unit 59 whereby the amplitude of the summed traces as a function of time is printable. Of more use as an output unit, however, is disk unit 60, which can temporarily store the data. Thereafter, an off-line digital plotter capable of generating a side-by-side display is used in conjunction with the data on the disk unit 60. Such plotters are available in the art, and one proprietary model that I am familiar with uses a computer-controlled CRT for optically merging onto photographic paper, as a display mechanism, the seismic data. Briefly, in such a plotter the seismic data, after summation, are converted to CRT deflection signals; the resulting beam is drawn on the face of the CRT and the optically merged record of the event indicated, say via photographic film. After a predetermined number of side-by-side lines have been drawn, the film is processed in a photography laboratory and hard copies returned to the interpreters for their review.

FIG. 11 illustrates CPU 51 and control unit 52 in more detail.

As shown, the CPU 51 includes an array of registers generally indicated at 62 tied to an ALU 63 through an internal data bus 64 under control of control unit 52. The registers 62 are temporary storage areas. Program counter 65 and instruction register 66 have dedicated uses; the other registers, such as accumulator 67, have more general uses.

The accumulator 67 usually stores one of the seismic operands to be manipulated by the ALU 63. E.g., in the summation of traces, the instruction may direct the ALU 63 to not only add in sequence the contents of the temporary registers containing predetermined trace amplitudes together with an amplitude value in the accumulator, but also store the result in the accumulator itself. Hence, the accumulator 67 operates as both a source (operand) and a destination (result) register. The additional registers of the array 62 are useful in manipulation of seismic data, since they eliminate the need to shuffle results back and forth between the external memory units of FIG. 10 and accumulator 67. In practice most ALU's also provide other built-in functions, including hardware subtraction, boolean logic operations, and shift capabilities. The ALU 63 also can utilize flag bits generated by FF unit 73 which specify certain conditions that arise in the course of arithmetical and logical manipulations. Flags typically include carry, zero, sign, and parity. It is possible to program jumps which are conditionally dependent on the status of one or more flags. Thus, for example, the program may be designed to jump to a special routine if the carry bit is set following an addition instruction.

Instructions making up the program for operations involving seismic data are stored in the program memory unit 53 of the CPU 51 of FIG. 11. The program is operated upon in a sequential manner except when instructions in the memory units 53, 54 call for special commands such as "jump" (or "call") instructions. While the program associated with the present invention is a relatively straightforward one, hence avoiding most "jump" and "call" instructions, "call" instructions for subroutines are common in the processing of seismic data and could be utilized, if desired. In "call" instructions, the CPU 51 has a special way of handling subroutines in order to insure an orderly return to the main program. When the processor receives a call instruction, it increments the program counter 65 and notes the counter's contents in a reversed memory area of the memory unit known as the "stack".

CPU's have different ways of maintaining stack contents. Some have facilities for the storage of return addresses built into the CPU itself. Other CPU's use a reversed area of external memory as the stack and simply maintain a "pointer" register, such as pointer register 70, FIG. 11, which contains the address of the most recent stack entry. The stack thus saves the address of the instruction to be executed after the subroutine is completed. Then the CPU 51 loads the address specified in the call into its program counter 65. The next instruction fetched will therefore be the first step of the subroutine. The last instruction in any subroutine is a "return". Such an instruction need specify no address.

Having now briefly described the operations of the CPU 51, Table I is presented below containing a full instruction set for its operations.

                                      TABLE I                                      __________________________________________________________________________     Summary of Processor Instructions By Alphabetical Order                                             Instruction Code.sup.1                                                                         Clock.sup.2                               Mnemonic                                                                             Description    D.sub.7                                                                          D.sub.6                                                                          D.sub.5                                                                          D.sub.4                                                                          D.sub.3                                                                          D.sub.2                                                                          D.sub.1                                                                          D.sub.0                                                                          Cycles                                    __________________________________________________________________________     ACI   Add immediate to A with                                                        carry          1 1 0 0 1 1 1 0 7                                         ADC M Add memory to A with carry                                                                    1 0 0 0 1 1 1 0 7                                         ADC r Add register to A with                                                         carry          1 0 0 0 1 S S S 4                                         ADD M Add memory to A                                                                               1 0 0 0 0 1 0 1 7                                         ADD r Add register to A                                                                             1 0 0 0 0 S S S 4                                         ADI   Add immediate to A                                                                            1 1 0 0 0 1 1 0 7                                         ANA M And memory with A                                                                             1 0 1 0 0 1 1 0 7                                         ANA r And register with A                                                                           1 0 1 0 0 S S S 4                                         ANI   And immediate with A                                                                          1 1 1 0 0 1 1 0 7                                         CALL  Call unconditional                                                                            1 1 0 0 1 1 0 1 17                                        CC    Call on carry  1 1 0 1 1 1 0 0 11/17                                     CM    Call on minus  1 1 1 1 1 1 0 0 11/17                                     CMA   Compliment A   0 0 1 0 1 1 1 1 4                                         CMC   Compliment carry                                                                              0 0 1 1 1 1 1 1 4                                         CMP M Compare memory with A                                                                         1 0 1 1 1 1 1 0 7                                         CMP r Compare register with A                                                                       1 0 1 1 1 S S S 4                                         CNC   Call on no carry                                                                              1 1 0 1 0 1 0 0 11/17                                     CNZ   Call on no zero                                                                               1 1 0 0 0 1 0 0 11/17                                     CP    Call on positive                                                                              1 1 1 1 0 1 0 0 11/17                                     CPE   Call on parity even                                                                           1 1 1 0 1 1 0 0 11/17                                     CPI   Compare immediate with A                                                                      1 1 1 1 1 1 1 0 7                                         CPO   Call on parity odd                                                                            1 1 1 0 0 1 0 0 11/17                                     CZ    Call on zero   1 1 0 0 1 1 0 0 11/17                                     DAA   Decimal adjust A                                                                              0 0 1 0 0 1 1 1 4                                         DAD B Add B & C to H & L                                                                            0 0 0 0 1 0 0 1 10                                        DAD D Add D & E to H & L                                                                            0 0 0 1 1 0 0 1 10                                        DAD H Add H & L to H & L                                                                            0 0 1 0 1 0 0 1 10                                        DAD SP                                                                               Add stack pointer to H & L                                                                    0 0 1 1 1 0 0 1 10                                        DCR M Decrement memory                                                                              0 0 1 1 0 1 0 1 10                                        DCR r Decrement register                                                                            0 0 D D D 1 0 1 5                                         DCX B Decrement B & C                                                                               0 0 0 0 1 0 1 1 5                                         DCX D Decrement D & E                                                                               0 0 0 1 1 0 1 1 5                                         DCX H Decrement H & L                                                                               0 0 1 0 1 0 1 1 5                                         DCX SP                                                                               Decrement stack pointer                                                                       0 0 1 1 1 0 1 1 5                                         DI    Disable interrupt                                                                             1 1 1 1 0 0 1 1 4                                         EI    Enable interrupts                                                                             1 1 1 1 1 0 1 1 4                                         HLT   Halt           0 1 1 1 0 1 1 0 7                                         IN    Input          1 1 0 1 1 0 1 1 10                                        INR M Increment memory                                                                              0 0 1 1 0 1 0 0 10                                        INR r Increment register                                                                            0 0 D D D 1 0 0 5                                         INX B Increment B & C registers                                                                     0 0 0 0 0 0 1 1 5                                         INX D Increment D & E registers                                                                     0 0 0 1 0 0 1 1 5                                         INX H Increment H & L registers                                                                     0 0 1 0 0 0 1 1 5                                         INX SP                                                                               Increment stack pointer                                                                       0 0 1 1 0 0 1 1 5                                         JC    Jump on carry  1 1 0 1 1 0 1 0 10                                        JM    Jump on minus  1 1 1 1 1 0 1 0 10                                        JMP   Jump unconditional                                                                            1 1 0 0 0 0 1 1 10                                        JNC   Jump on no carry                                                                              1 1 0 1 0 0 1 0 10                                        JNZ   Jump on no zero                                                                               1 1 0 0 0 0 1 0 10                                        JP    Jump on positive                                                                              1 1 1 1 0 0 1 0 10                                        JPE   Jump on parity even                                                                           1 1 1 0 1 0 1 0 10                                        JPO   Jump on parity odd                                                                            1 1 1 0 0 0 1 0 10                                        JZ    Jump on zero   1 1 0 0 1 0 1 0 10                                        LDA   Load A direct  0 0 1 1 1 0 1 0 13                                        LDAX B                                                                               Load A indirect                                                                               0 0 0 0 1 0 1 0 7                                         LDAX D                                                                               Load A indirect                                                                               0 0 0 1 1 0 1 0 7                                         LHLD  Load H & L direct                                                                             0 0 1 0 1 0 1 0 16                                        LXI B Load immediate register                                                        Pair B & C     0 0 0 0 0 0 0 1 10                                        LXI D Load immediate register                                                        Pair D & E     0 0 0 1 0 0 0 1 10                                        LXI H Load immediate register                                                        Pair H & L     0 0 1 0 0 0 0 1 10                                        LXI SP                                                                               Load immediate stack                                                           pointer        0 0 1 1 0 0 0 1 10                                        MVI M Move immediate memory                                                                         0 0 1 1 0 1 1 0 10                                        MVI r Move immediate register                                                                       0 0 D D D 1 1 0 7                                         MOV M,r                                                                              Move register to memory                                                                       0 1 1 1 0 S S S 7                                         MOV r,M                                                                              Move memory to register                                                                       0 1 D D D 1 1 0 7                                         MOV r.sub.1,r.sub.2                                                                  Move register to register                                                                     0 1 D D D S S S 5                                         NOP   No operation   0 0 0 0 0 0 0 0 4                                         CRA M Cr memory with A                                                                              1 0 1 1 0 1 1 0 7                                         ORA r Or register with A                                                                            1 0 1 1 0 S S S 4                                         ORI   Or immediate with A                                                                           1 1 1 1 0 1 1 0 7                                         OUT   Output         1 1 0 1 0 0 1 1 10                                        PCHL  H & I to program counter                                                                      1 1 1 0 1 0 0 1 5                                         POP E Pop register pair B & C                                                        off stack      1 1 0 0 0 0 0 1 10                                        POP D Pop register pair D & E                                                        off stack      1 1 0 1 0 0 0 1 10                                        POP H Pop register pair H & L                                                        off stack      1 1 1 0 0 0 0 1 10                                        POP PSW                                                                              Pop A and Flags off stack                                                                     1 1 1 1 0 0 0 1 10                                        PUSH B                                                                               Push register Pair B & C                                                       on stack       1 1 0 0 0 1 0 1 11                                        PUSH D                                                                               Push register Pair D & E                                                       on stack       1 1 0 1 0 1 0 1 11                                        PUSH H                                                                               Push register Pair H & L                                                       on stack       1 1 1 0 0 1 0 1 11                                        PUSH PSW                                                                             Push A and Flags on stack                                                                     1 1 1 1 0 1 0 1 11                                        RAL   Rotate A left through                                                          carry          0 0 0 1 0 1 1 1 4                                         RAR   Rotate A right through                                                         carry          0 0 0 1 1 1 1 1 4                                         RC    Return on carry                                                                               1 1 0 1 1 0 0 0 5/11                                      RET   Return         1 1 0 0 1 0 0 1 10                                        RLC   Rotate A left  0 0 0 0 0 1 1 1 4                                         RM    Return on minus                                                                               1 1 1 1 1 0 0 0 5/11                                      RNC   Return on no carry                                                                            1 1 0 1 0 0 0 0 5/11                                      RNZ   Return on no zero                                                                             1 1 0 0 0 0 0 0 5/11                                      RP    Return on positive                                                                            1 1 1 1 0 0 0 0 5/11                                      RPE   Return on parity even                                                                         1 1 1 0 1 0 0 0 5/11                                      RPO   Return on parity odd                                                                          1 1 1 0 0 0 0 0 5/11                                      RRC   Rotate A right 0 0 0 0 1 1 1 1 4                                         RST   Restart        1 1 A A A 1 1 1 11                                        RZ    Return on zero 1 1 0 0 1 0 0 0 5/11                                      SBB M Subtract memory from A                                                         with borrow    1 0 0 1 1 1 1 0 7                                         SBB r Subtract register from A                                                       with borrow    1 0 0 1 1 S S S 4                                         SBI   Subtract immediate from A                                                      with borrow    1 1 0 1 1 1 1 0 7                                         SHLD  Stcre H & L direct                                                                            0 0 1 0 0 0 1 0 16                                        SPHL  H & L to stack pointer                                                                        1 1 1 1 1 0 0 1 5                                         STA   Store A direct 0 0 1 1 0 0 1 0 13                                        STAX B                                                                               Store A indirect                                                                              0 0 0 0 0 0 1 0 7                                         STAX D                                                                               Store A indirect                                                                              0 0 0 1 0 0 1 0 7                                         STC   Set carry      0 0 1 1 0 1 1 1 4                                         SUB M Subtract memory from A                                                                        1 0 0 1 0 1 1 0 7                                         SUB r Subtract register from A                                                                      1 0 0 1 0 S S S 4                                         SUI   Subtract immediate from A                                                                     1 1 0 1 0 1 1 0 7                                         XCHG  Exchange D & E, H & L                                                          Registers      1 1 1 0 1 0 1 1 4                                         XRA M Exclusive Or memory                                                            with A         1 0 1 0 1 1 1 0 7                                         XRA r Exclusive Or register                                                          with A         1 0 1 0 1 S S S 4                                         XRI   Exclusive Or immediate                                                         with A         1 1 1 0 1 1 1 0 7                                         XTHL  Exchange top of stack,                                                         H & I          1 1 1 0 0 0 1 1 18                                        __________________________________________________________________________      .sup.1 DDD or SSSOOOB-001C-010D-011E-100H-101L-110 Memory111A.                 .sup.2 Two possible cycle times (5/11) indicate instruction cycles             dependent on condition flags.                                            

EXAMPLES

Diagnostic capability provided by the method of the present invention is better illustrated in the Examples set forth below.

EXAMPLE I

Seismic data were obtained over a gas field near Sacramento, Calif. These data, in CDP-stacked form, are shown in FIG. 12. The field, discovered in 1972, consists of a 100-foot sand which is almost fully gas-saturated. The discovery well is located at about SP-86 of FIG. 12, with the currently developed portion of the field extending from about SP-75 to SP-115. Gas occurs at a depth of about 7000 feet, which corresponds to a time of about 1.75 seconds on the plot.

Common-depth-point gathers from 3 locations, A, B and C of FIG. 12, are shown in FIGS. 13(a), 13(b) and 13(c). Both single-fold and 10-fold summed gathers are shown for locations A and B, while only the summed gather is shown for location C. Shot-to-group offset for all gathers increases to the left, as indicated with the minimum and maximum trace offset distances annotated. These distances change on the summed gathers because the summing is done over 4 offsets.

Note the strong amplitude increase with increasing offset at locations A and B. The 10-fold summing obviously improves signal-to-noise ratios and an amplitude increase by a factor of about three is indicated from near to far offset. Gathers at location C, however, show no indication of amplitude increase with offset, and in fact show a decrease. This possibly indicates an absence of gas in the vicinity of location C. This possibility is also supported by the presence of a gas-water contact in a well structurally projected at about SP-120.

EXAMPLE II

Seismic data were obtained in the Fallon Basin of Nevada and are depicted in CDP-gathered format in FIG. 14. A well was drilled at SP-127 in FIG. 14. A seismic amplitude anomaly is indicated at location A at about 1.6 seconds. Upon drilling, the amplitude anomaly was found to originate from two basaltic layers, 100 feet and 60 feet in thickness. As its structural position indicates, this well was a stratigraphic test in an undrilled basin.

The common-depth-point gathers at the well location are shown in FIG. 15. Here, there is a strong indication of reflection amplitude decrease with increasing offset. This finding is consistent with the absence of gas in the geologic section and the expected Poisson's ratios for sediments and basalt.

EXAMPLE III

Seismic data obtained from an area in the Sacramento Valley, Calif., are depicted in FIG. 16. A well was drilled at SP-61. Note the amplitude anomaly extending from about SP-45 to about SP-90 at 1.5 seconds. However, the amplitude anomaly was found to originate from a high-velocity conglomerate layer.

Shown in FIGS. 17(a) and 17(b) are the single-fold common-depth-point gathers at two locations: location A at the well and location B, about 1/2 mile to the west. The gathers at location A do indeed indicate the absence of gas, i.e., no noticeable increase in reflector amplitude with offset. However, the gathers at location B do show a slight increase in amplitude with offset, i.e., possible gas.

EXAMPLE IV

Seismic data were obtained for another area and are depicted in FIG. 18. The possible gas-related amplitude anomalies are located (i) between SP-270 and -310 at about 1.3 seconds and (ii) between SP-250 and -300 at about 1.0 second.

The ten-fold CDP gathers at locations A and B of FIG. 18 are shown in FIGS. 19(a) and 19(b), respectively. Here, there do indeed appear to be indications of amplitude increase with offset. In FIG. 19a, the anomaly appears over a region where amplitude increases with offset. In FIG. 19b, the anomaly at 1.0 seconds is thought to be related to low-velocity shale.

EXAMPLE V

Seismic data were obtained for another area and are depicted in FIG. 20. The geologic section was limestone embedded in shale. The gas-related anomaly is located over the indicated rectangular area of the Figure.

Here, note that for this lithology, gas is indicated by decreases in amplitude with offset, as shown in FIG. 21 representing CDP gathers at surface locations 102 and 103 of FIG. 20, as viewed respectively from right to left in FIG. 21.

The method of the present invention as described provides a geophysicist with a strong tool for differentiating gas-filled and non-gas reservoirs in a variety of structural combinations, e.g., sand and limestone embedded in shale.

MODIFICATION

However, while the foregoing embodiments have emphasized processing techniques which may be more suitable for processing centers remote from the field site, there are situations in which on-site processing is desirable.

FIGS. 22-25 illustrate a system for such purpose.

As shown in FIG. 22, a digital field system is schematically indicated at 100. Purpose of system 100: to indicate--at a field site--gas-containing strata within an earth formation 120 based on the strategy that such strata has a low Poisson's ratio and its acoustic contrast with the overburden rock is surprisingly effected as a function of the angle of incidence of the propagating seismic wave, viz., a significant--and progressive--change in P-wave reflection coefficient occurs as a function of the angle of incidence as the seismic data is collected. The field system 100 is associated with a seismic data-gathering truck (not shown), the latter being movable in the direction of survey, say in the direction of arrow A, and includes field control and analyzer system 111. System 111 is interconnected between digital firing system 112 and a series of remote digital acquisition and telemetering circuits 113 called "RDATC's". Each RDATC 113, in turn, is connected to several geophone flyer groups 114, say at least four per RDATC, each flyger group 114 being composed of two or more geophone flyers 115. The flyer groups 114 form a geophone spread which is usually two or more miles in length.

Digital firing system 112 controls a vibrator 116 or dynamite or any energy source located at the earth's surface or therebelow. Assuming a vibrator is used, it is preferably a hydraulic-type vibrator, such as provided in a Vibroseis system, a trademark of Continental Oil Company, and provides for the initiation of a control seismic energy signal through amplifiers 117 for transference into the earth formation 120 below the RDATC's 113 and flyer groups 114, say at a source point (SP). The acoustic wave front from the energy source inparted into the formation 120 is in accordance with the predetermined variation (amplitude versus time) of a pilot signal obtained from digital firing system 112 in a conventional manner.

After the vibrator (or other energy source) has been initiated, a collection cycle occurs; during the first collection cycle, reflections of the seismic energy such as from discontinuity 121 are detected by the geophone spread, viz., by geophone flyer groups 114 associated with geographic stations A, B, C, D, E, etc. The analogue output of each geophone flyer groups 114 (and hence stations A, B, C, D, E, etc.) is fed in turn to one or a series of RDATC's 113. Since the output of each flyer groups 114 is a single combined electrical signal, a separate channel of each RDATC 113 is used to receive this data.

Within the RDATC 113, each channel of data undergoes a series of operations, including digitization, formatization and storage until the time is ripe for the bits of information to be transmitted (telemetered) back to the recording truck, i.e., to control and analyzer system 111. Since the data from all RDATC's 113 is storable, the information can be fed--on command--say, along a single two-conductor cable 90, in a series format to the field control and analyzer system 111 where finalized processing and display occurs. Of course, instead of cable 90, other means could be used to transfer the data from each RDATC to the system 111, say, via a radio link.

After the vibrator 116 (or any other energy source) has operated at source point (SP), the vibrator 116 (or other energy source) as well as portions of the geophone spread, i.e., flyer groups 114 associated with say station A may be displaced in new positions in the direction of arrow A.

Assume the vibrator (or other source) is located in new source point (SP') displaced in the direction of arrow A an inline distance (d) from its previous locations (SP). The geophone spread can be advanced the same inline distance (d), say where d is equal to the total length of a flyer group that comprise a given station. At that time, a new collection cycle begins in the manner previously described.

Of course, the geophone spread of FIG. 22 can comprise a great number of geophone flyer groups 114 depending inter alia, on the number of active RDATC's that are used in the field, the sampling rate used at each RDATC, and degree of difficulty in differentiating high-intensity anomalies of non-gas and gas-containing strata. Since the channel capacities of the RDATC's are additive, as many as 384 channels of information can be recorded at the field analyzer system 111. But conventionally about 28 RDATC's are used in one field arrangement; assuming a sampling rate of roughly 4 milliseconds allows about 112 channels of data to be easily processable; but only about 96 are selected for seismic recording; the remainder, about 16 channels, are usually used for documentational purposes.

FIG. 23 illustrates the groups 114 in more detail.

As shown, station A is seen to be associated with flyer group 114a, viz., flyers 115a and 115b. Similarly, station B is associated with the flyer group 114b composed of flyer pair 115c and 115d; while station C is associated with flyer group 114c comprising flyers 115e and 115f. Finally, station D is associated with flyer group 114d consisting of flyer pair 115g and 115h.

Flyers of each pair, i.e., flyers 115a, 115b, . . . 115g, 115h, are electrically joined at a series of central connectors 130, i.e., each of the connectors 130 includes separate pairs of connectors 130a, 130b, 130c, 130d, 130e, 130f, 130g and 130h formed at the point of electrical connection of each of the flyer pairs. Note also that each central connector 130 is coincidentally located with the composite geographical position associated with each respective station A, B, C, D, E . . . etc.

Additionally, between each adjacent pair of stations, i.e., between stations A, B and C, D, is a second series of electrical connectors 131 for the flyers, viz., paired connectors 131a, 131b and 131c, 131d.

Although mechanically connectors 130 and 131 are similar, electrically each is independent of the other. That is to say, the main function of connector 130 is to sum the electrical signal output of each flyer pair of each geophone group 114a, 114b . . . 114d of FIGS. 23, while the main function of the other connector 131 is to isolate the signal output from adjacent flyer groups; but connector 131 also allows the output signal from the more remote flyer groups, i.e., flyer groups 114a and 114d to gain entry to the more near flyer groups 114b and 114c, respectively, for eventually feeding to the RDATC 113a.

FIG. 24 illustrates RDATC 113a in still more detail.

As shown, RDATC 113a includes a series of input channels 140. Each of the channel 140 discretely connects to an output of flyer groups 114a, 114b . . . 14d. The signal output from the above-mentioned flyer groups first passes from a channel 140 through filter 141, amplifier 142 to multiplexer network 143. Within the multiplexer network 143, the seismic data received at each flyer groups almost instananeously is multiplexed and is passed through gain logic circuit 144 to A/D convertor 145. The function of the former is to make sure that at A/D convertor 145 is within its processing capability. Within the A/D convertor 145, the analogue information is converted to a digital value after which it passes to format logic circuit 146.

Note that format logic circuit 146 is controlled through a master clock circuit 147. The latter receives a control signal from the control and analyzer system 111 of FIG. 22; such signal passes through transmit/receive circuit 148 to the circuit 147 to either start/stop operations as well as pace the operations of the associated circuits. In regard to the latter, note that clock circuit 147 is also associated with operation of analogue control circuit 149 connected to not only A/D convertor 145 but also to gain logic circuit 144 and multiplexer network 143. In this way, data passing through multiplexer network 143, gain logic circuit 144 and A/D convertor 145 does so on a controlled pace basis so that the data length at format logic circuit 146 is correct.

The format logic circuit 146 includes a series of registers, not shown. Within these registers, the seismic information associated with each of the stations A, B . . . D is stored. But such data is subject to being called--on command--to the digital recording and control system 111 of FIG. 22 as previously mentioned. All such signals are exact multiples of the signals at clock circuit 147. So read-out of the data within format logic circuit 146 is accomplished at specific intervals of time that are exact multiples of the clock pulse, once a start/send signal has been received at the RDATC 113a.

Note in FIG. 24 that the combination output/input of transmit/receive circuit 148 is the single two-conductor cable 90 of FIGS. 22 and 23. Each flyer group 114 comprising the flyer groups 114a, 114b, 114c and 114d, must be properly connected in both mechanical and electrical senses to insure proper flyer and system operation.

FIG. 25 illustrates control and analyzer system 111 in more detail.

As shown, system 110 has an input/output channel 150. The data from each RDATC sequential flows via the channel 150 through transmitter/receiver 151 and thence through buffer 152, static and dynamic corrector 153, format logic buffer 154, D/A convertor 155 to recorder/display means 156.

Buffer 152 allows the packing of several digital words into a memory word as well as increases data flow rates into static and dynamic corrector 153, as required. It is to be recognized that the corrector 153 requires comparisons be made between common events of adjacent traces; consequently it is preferable to provide corrector 153 with a serial-to-parallel convertor and memory means (not shown) operating under control of control logic 157 through program counter 158 and clock 159.

Control of operations is conventional: clock 159, program counter 158 and control logic 157 synchronize operations. As the data enters via transmitter-receiver 151, the address of each data word (amplitude and time) is known as a function of offset (detector, source point and center point), profile line number, common offset line number, common counterpoint line number and common detector location line number. Reason: the array and source geometry remain constant from RDATC-to-RDATC; hence serial position of the data from each RDATC is related in a known manner to the above-named variables. And, the pacing of the operations via clock 159, counter 158 and control logic circuit 157 is likewise constant from RDATC-to-RDATC and but not from element-to-element within the system 111.

Note also that logic control circuit 157 also gates the data relative to static and display corrector 153 via buffers 152 and 154 as well as controls the digital-to-analog conversion at convertor 155 and the display at display-recorder 156.

Since the data to be displayed at display 156a places emphasis on centerpoint location in a two-dimensional coordinate system, viz., in a X-Y domain (with the additional use of oblique diagonals therethrough as set forth hereinbefore) and the third dimension is reserved for processing of the amplitude-to-time traces, the analysis of the final display for the presence of gas (i.e., amplitude variations as a function of offset) is easily accommodated.

Enchancement of adjacent traces by summation about adjacent common offset and common centerpoint axes, is likewise easily controlled via control logic circuit 157 in association with counter 158 and clock 159.

The invention is not limited to the above combinations alone, but is applicable to other anomalous circumstances as known to those skilled in the art. It should thus be understood that the invention is not limited to any specific embodiments set forth herein, as variations are readily apparent, and thus the invention is to be given the broadest possible interpretation within the terms of the following claims. 

What is claimed is:
 1. An on-site field method for increasing resolution of seismic records containing high-intensity amplitude events in order to associate such events with gas-bearing strata in the earth, comprising the steps of:(a) generating seismic field data, including a record of signals from acoustic discontinuities associated with said strata of interest by positioning and employing an array of sources and detectors such that centerpoints between selected pairs of sources and detectors form a series of centerpoints along a line of survey, said recorded signals being the output of said detectors; (b) by means of automated on-site processing means, statically and dynamically correcting said recorded signals to form corrected traces whereby each of said corrected traces are associated with a centerpoint horizontally midway between a source-detector pair from which said each corrected trace was originally derived; (c) by means of automated on-site processing means, formatting said corrected traces in two dimensions whereby each of said corrected traces is identified in its relationship to neighboring traces on the basis of progressive changes in horizontal offset value versus progressive changes in common centerpoint location, and (d) displaying a series of said traces of step (c) on a side-by-side basis as a function of progressively changing horizontal offset values, said displayed traces all being associated with at least the same general common group of centerpoints whereby progressive change in a high-intensity amplitude event from trace to trace of said displayed traces as a function of progressive change in horizontal offset value can be identified on-site, said progressive change being associable with strata containing gaseous hydrocarbons.
 2. The method of claim 1 in which step (c) is further characterized by the substeps of:(i) selecting a first series of traces associated with a group of progressively increasing common offset, common centerpoint locations; and (ii) summing said first series of selected traces to form a summed trace.
 3. The method of claim 2 with the additional substeps of:(iii) choosing a second series of traces associated with another group of common offset locations; and (iv) summing the second series of selected traces to form a second summed trace.
 4. The method of claim 3 in which step (d) is a side-by-side display of said summed traces as a function of progressively changing composite horizontal offset values whereby progressive changes in said high-intensity amplitude event is more easily identifiable.
 5. An on-site field method for converting an original multitrace seismic record into an improved section having increased resolution as to the nature of high-intensity amplitude events related to reflections from subsurface strata possibly containing gaseous hydrocarbons, said improved section being composed of a plurality of amplitude-versus-horizontal offset-and-time traces, said original record consisting of a plurality of multitrace seismic traces of amplitude-versus-horizontal coordinate-and-time, each of said traces constituting energy derived in association with a particular source-detector pair of known horizontal offset and of known centerpoint locations, and representing, in part, event reflections from said subsurface strata, said conversion comprising the steps of:(a) classifying on-site said original traces on the basis of common but progressively changing horizontal offset values and common but progressively changing common centerpoint locations, whereby each trace is identified by a centerpoint location common to at least another trace and a known horizontal offset value; and (b) displaying at least said each trace and said another trace associated with said common centerpoint location, as a function of progressively changing horizontal offset values to form at least a segment of said improved section whereby progressive change in a high-intensity amplitude event common to said each trace and said another trace as a function of progressive change in horizontal offset forming said segment of said improved section, can be identified on-site, said progressive change being associable with strata containing gaseous hydrocarbons.
 6. The method of claim 5 in which said common centerpoint location of said another associated trace of step (a) is also common to a plurality of additional other traces, each having known but progressively changing horizontal values with respect to said another trace.
 7. The method of claim 6 in which the step (b) is a side-by-side display of said each trace, said another trace and said additional other traces as a function of progressively changing horizontal offset value to form said improved section whereby progressive change in said high-intensity event is more easily identifiable. 